User's Manual

ManualsBrandsWulfsberg Electronics Division ManualsElectronicsVHF ATC Communication Transceiver

APPLICATION REVISIONS

REV

NEXT ASSEMBLY FINAL ASSEMBLY REV DESCRIPTION DATE APPROVED APPROVED

A Initial Release per DCN W3749 6-18-04 V Wallace J Markham

B Revised per DCN W3905 12-23-04 V Wallace J Markham

C Revised per DCN W4435 4-30-04 V Wallace J Markham

D Revised per DCN W4917 12-21-05 V Wallace Bob Evans

DWG. NO.

150-047012

THIS DOCUMENT CONTAINS PROPRIETARY INFORMATION OF WULFSBERG ELECTRONICS, A

CHELTON GROUP COMPANY, NEITHER RECEIPT NOR POSSESSION THEREOF CONFERS ANY RIGHT

TO REPRODUCE OR USE, OR DISCLOSE, IN WHOLE OR IN PART, ANY SUCH INFORMATION WITHOUT

WRITTEN AUTHORIZATION FROM WULFSBERG ELECTRONICS

APPROVALS DATE

DRAWN

C Gregory

6-18-04

CHECKED

H Schnieder

6-18-04

PILOT'S GUIDE, AVIONICS SYSTEMS,

FLITELINE ™

ENGINEER

J Markham

6-18-04

ISSUED

V Wallace

6-18-04

SIZE

CAGE CODE

1B7G3

DWG NO.

150-047012

REV

Typed signatures indicate approval. Handwritten signature

approval of this document is on file at Wulfsberg Electronics,

Prescott, Arizona.

SCALE: NONE DO NOT SCALE DRAWING

Summary of content (69 pages)

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FINAL ASSEMBLY D REVISIONS REV DESCRIPTION DATE APPROVED APPROVED A Initial Release per DCN W3749 6-18-04 V Wallace J Markham B C D Revised per DCN W3905 Revised per DCN W4435 Revised per DCN W4917 12-23-04 4-30-04 12-21-05 V Wallace V Wallace V Wallace J Markham J Markham Bob Evans DWG. NO.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE Table of Contents INTRODUCTION....................................................................................................................................................4 FLITELINE VHF COMMUNICATION SYSTEM (FLITECOMM)............................................................................5 GENERAL DESCRIPTION CVC-151..........................................................................................................................
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE FLITELINE ATC TRANSPONDER SYSTEM (FLITEXPDR) ..............................................................................53 GENERAL DESCRIPTION CTR-352 ........................................................................................................................ 53 CTR-352 CONTROLS (ARINC-410 OCTAL INTERFACE)......................................................................................... 55 OPERATING THE CTR-352 ...................................
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE Introduction The FliteLine™ Avionics Systems represent the next generation of Chelton avionics. The FliteLine Control Display units are subsystems of the Chelton Avionics FliteLine Systems. The FliteLine NAV/COM/ADF/ATC Control Displays are one of several methods of controlling the Chelton Avionics FliteLine remote-mounted avionics systems.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE FliteLine VHF Communication System (FliteCOMM) General Description CVC-151 The FliteLine CVC-151 is an all digital DSP VHF Comm Transceiver, built and designed to ARINC Air Transport specifications. The Transceiver is designed to meet the latest ATC environment, all future CNS ATN requirements, and has provisions for VDL Mode 2 and VDL Mode 3. The CVC-151 features a 20 watt solid-state transmitter, is compliant with 25 kHz or 8.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE The CVC-152 Communication Control Display Unit is designed to interface with Chelton FliteLine Communications Radios (CVC-151), Chelton Series III Communications Radios (VC-401B and VC-401C in the VCS 40 Systems), and Collins Communication Radios with the ARINC 410 (2x5) Interfaces. Page 6 Dec 2005 Publication No. 150-047012 Rev.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CVC-152 Control Display Unit CHELTON COM "Active" COM Annunciator COM System Number COM Transmit Annunciator ACT 12 124.950 Volume Annunciator TX 124.950 Mode Annunciators Standby COM Frequency Mode Select (Outer Knob) Volume Control (Inner Knob) Active COM Frequency 25k MODE VOL 8.33k 1MHz Frequency Tuning (Outer Knob) TST TUNE PWR 25kHz and 8.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CVC-152 Control Display Unit CHELTON COM "Active" COM Annunciator COM System Number COM Transmit Annunciator ACT 12 TX Volume Annunciator 124.950 Mode Annunciators 124.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CVC-152 Controls (Series III, FliteLine, ARINC 410 Interfaces) CHELTON ACT 1 Mode Selector COM Switchable Channel Spacing 25k - Selects 25 kHz channel spacing. 124.950 8.33k - Selects 8.33 kHz channel spacing. 124.950 25k 8.33k TST MODE VOL Outer Knob TST - Disables the squelch circuits to allow audible verification of receiver operation. TUNE *Note: There is no ON mode when 25kHz and 8.33kHz capable Radios are detected.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CVC-152 Controls (Series III, FliteLine, and ARINC 410 Interfaces Continued…) CHELTON ACT 1 Frequency Knobs COM The right outer knob tunes the transmit/receive frequency in whole MHz steps (118, 119, 120, etc.). The right inner knob tunes in 25 or 8.33 kHz steps (refer to the table on page 10). 124.950 Frequency Transfer Button 124.950 25k 8.33k The right inner knob also functions as a pushbutton for switching the active and standby frequency.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CVC-152 Controls (Series III, FliteLine, and ARINC 410 Interfaces Continued…) Active Frequency ACT 1 124.950 25k 8.33k The upper line of the display always shows the active frequency… TST Active Annunciator ACT 1 124.950 …which is indicated by the Active Annunciator (the letters ACT). 124.950 25k 8.33k TST Standby Frequency ACT 1 124.950 The lower line of the display shows the standby frequency. 124.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CVC-152 Controls (Series III, FliteLine, and ARINC 410 Interfaces Continued…) System Number ACT 1 124.950 TX 124.950 25k 8.33k TST The System Number indicates that this display is for COM System 2 (when more than one system is installed). The number 1 indicates that this display is for COM System 1 (when more than one system is installed).
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE Operating the CVC-152 1. Turn the MODE SELECTOR to ON (fixed channel spacing) or to 25kHz or 8.33kHz (switchable channel spacing). The last frequencies selected prior to System turnoff reappear in the display. 2. If these are not the desired frequencies, rotate the appropriate FREQUENCY KNOB until the desired frequency is displayed as the standby frequency in the lower line of the display.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE 3. Press and release the FREQUENCY TRANSFER button. This exchanges the two displayed frequencies. The desired frequency is now active and may be used immediately. 4. Use the VOLUME CONTROL to adjust volume if a station is broadcasting. 5. To set a new standby frequency, rotate the appropriate FREQUENCY KNOB until the desired frequency is displayed in the lower line of the display.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CVC-152 Notes 1. The FREQUENCY SELECTOR knobs tune the radio transceiver directly. The display shows the frequencies to which the radio transceiver is actually tuned. In addition to the CVC-152, the Chelton Series III transceivers may also be tuned by an ARINC 429 digital bus. In addition to the CVC-152, the Chelton FliteLine transceivers may be tuned by either ARINC 429 digital bus or Controller Area Network (CAN) Bus. 2.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE VHF COM System Block Diagram (Typical) VHF Antenna ARINC 429 Radio Management System VHF Communications Tranceiver Microphone Audio and PTT Audio Panel Function Select Audio Tuning Data* Panel Dimmer Control FrequencySelect Sidetone CVC-152 Audio Display Dimmer Control * Control Displays configured for ARINC 410 typically do not have tuning data returned from the radio Page 16 Dec 2005 Publication No. 150-047012 Rev.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE FliteLine VHF Navigation System (FliteNAV and FliteDME) General Description CVN-251 The FliteLine CVN-251 is an all digital DSP Navigation System which combines VOR/LOC, Glideslope and Marker Beacon functions. This Receiver configuration supports the total navigation interface requirements for MFD or moving map displays.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE General Description CVN-252 The Chelton CVN-252 VHF Navigation Control Display is designed to control VHF navigation receiving systems that combine VOR/LOC, glideslope, and marker beacon reception. The CVN-252 is a direct replacement for the Chelton CD-412B Control Display Unit. The CVN-252 Control Display can digitally display BEARING TO or RADIAL FROM any selected VOR station.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CVN-252 NAV Control Display CHELTON NAV "Active" NAV Annunciator NAV System Number ACT 12 Active NAV Frequency Volume Annunciator 110.20 Mode Annunciators 108.15 Standby NAV Frequency, Bearing, and Radial ON Mode Select (Outer Knob) Volume Control (Inner Knob) Power On/OFF (pushbutton) Publication No. 150-047012 Rev.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CVN-252 Controls (Series III and FliteLine Interface) CHELTON ACT 1 Mode Selector NAV ON - The last frequencies displayed reappear on the display. Allows tuning of active and standby frequencies. 110.20 RAD - Displays the radial the aircraft is on from the selected VOR. It is displayed digitally below the selected VOR frequency. 108.15 ON MODE VOL Outer Knob Page 20 Dec 2005 PWR RAD BRG BRG - Displays the bearing to the selected VOR.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CVN-252 Controls (Series III and FliteLine Interface continued…) CHELTON ACT 1 Frequency Selector NAV The right outer knob tunes the receiver in whole MHz steps (108, 109, 110, etc., up to 117 MHz). 110.20 The right inner knob tunes fractional MHz frequencies in 50 kHz steps (.00, .05, .10, .15, etc., up to .95). 108.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CVN-252 Controls (Series III and FliteLine Interface continued…) ACT 1 When the NAV radio is turned on, the last display before turnoff is displayed again. 110.20 The upper line of the display always shows the active frequency (indicated by the letters ACT. The lower display may show the standby frequency, digital radial or bearing, or LOC annunciation, depending on the FUNCTION SELECTOR setting. 108.15 ON ACT 1 RAD BRG 111.40 084.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CVN-252 Controls (Series III and FliteLine Interface continued…) ACT 1 111.40 Three dashes on the bottom line indicate a flag condition. This flag means that RAD or BRG has been selected on the FUNCTION SELECTOR switch but cannot be displayed because of insufficient signal or during VOR station passage. --ON ACT 1 RAD BRG 111.40 L0C ON ACT 1 RAD When the top (active) frequency is a localizer station, bearing or radial cannot be displayed.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CVN-252 Controls (Series III and FliteLine Interface continued…) ACT 2 111.40 264.0° ON RAD The number 2 below the letters ACT represent Nav System 2 when more than one Nav System is installed. This number is fixed at the time of installation. A blank below the letters ACT represent either Nav System 3 (when more than 2 Nav Systems are installed) or that only one Nav System is installed.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CVN-252 Controls (Series III and FliteLine Interface - DME Hold Operation) CHELTON HLD – (optional) By switching to this mode and momentarily pressing the right inner pushbutton system will activate or deactivate DME Hold. Indication of DME. NAV ACT 1 110.20 * When the mode selector knob is placed on the HLD mode a left arrow will appear indicating off-screen modes to the left.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CVN-252 Controls (ARINC 410 Interface) CHELTON ACT 1 ON – Normal Operation Mode NAV TST – In TST (Test) mode the Control Display will send a discrete signal to the radio to enter test mode or self test mode. 110.20 108.15 ON MODE VOL • Refer to operation manual for the installed radio for further guidance on test and self test mode. • Volume control, power, and frequency operations are the same as Series II and FliteLine configured units.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CVN-252 Controls (ARINC 410 Interface - DME Hold Operation) CHELTON ACT 1 HLD – (optional) By switching to this mode and momentarily pressing the right inner pushbutton system will activate or deactivate DME Hold. Indication of DME. NAV 110.20 The standby frequency will dash when in HLD mode and tuning the active frequency is inhibited. ---.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE Operating the CVN-252 1. Set the MODE SELECTOR to ON. 2. If these are not the desired frequencies, rotate the FREQUENCY KNOBS until the desired frequency is displayed on the bottom portion of the display 3. Press and release the FREQUENCY TRANSFER button. This exchanges the two displayed frequencies. The desired frequency is now active and may be used immediately. 4. Adjust the VOLUME CONTROL for the desired audio level. 5.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CVN-252 Notes 1. The FREQUENCY SELECTOR KNOBS tune the navigational radio receiver directly. The Series III and FliteLine radios digitally transmit the actual frequency to which the receiver is tuned. The transceiver may also be tuned by an external ARINC 429 digital data bus. 2. The VOLUME control on the CVN-252 Control Display does not adjust the volume of the Marker Beacon receiver in the navigation receiver. This volume is preset.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE General Description SD-442 The SD-442 is a panel mounted DME Selector Display providing the pilot the means to control the CDM-451 modes and to display DME information. The unit provides a full time display of distance and ground speed to either the NAV 1 or NAV 2 selected VORTAC. Annunciation of the active NAV system is displayed below the distance readout.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE The SD-442 has only three controls. Each is a momentary, spring-loaded type that releases when finger pressure is removed. On-off power is through an external switch such as a radio or avionics master switch, or a dedicated DME switch. Volume control of DME station identification audio is also external, typically located on an audio panel. NAV - Alternately places annunciator 1, 2, or RNV in display. 1 - Selects NAV System 1 as the controller of the DME channel.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE TTS - (Time-To-Station) While this switch is held pressed, time-to-station will be shown on the display above the switch. When the switch is released, the display returns to its previous readout of ground speed. If in hold when the TTS switch is pressed, the HLD FREQ on the display will blink twice to alert the pilot. NOTE: When DME is being tuned by an MLS, receive DME hold is inhibited. Page 32 Dec 2005 Publication No. 150-047012 Rev.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE VHF NAV System Block Diagram (Typical) Glide Slope Antenna VOR/Localizer Antenna Marker Beacon Antenna Marker Beacon Lamps LO HI ARINC 429 Channel Select DME Marker Beacon Sensitivity VHF Navigation Receiver NAV Data Output ARINC 429 Freq.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE FliteLine Automatic Direction Finder (ADF) General Description The Chelton CDF-552 ADF Control Display provides control to Automatic Direction Finding radios enabling reception of low-frequency navigational aids and AM broadcast stations in the 190.0 – 1860 kHz frequency range. The CDF-552 provides a direct replacement of the Series III CD-432B Control Display Unit, for control of the DF-431B in the DFS-43A system.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CDF-552 Control Display Unit CHELTON ADF "Active" ADF Annunciator ADF System Number ACT 12 Standby ADF Frequency and Bearing Volume Annunciator 190.5 Mode Annunciators 1860.0 ANT Mode Select (Outer Knob) Active ADF Frequency MODE VOL Volume Control (Inner Knob) ADF BRG TUNE 100kHz Frequency Tuning (Outer) 10kHz and .5 kHz Frequency Tuning (Inner Knob) PWR Power On/OFF, Whole/Half kHz (pushbutton) Publication No. 150-047012 Rev.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CDF-552 Controls (Series III and FliteLine Interface) Mode Selector CHELTON ADF ACT 1 ANT - Enables the ADF System and the non-directional sense antenna. The last frequencies displayed reappear on the display. Frequency tuning is enabled, but no direction-finding capability exists in this mode. External pointers park at 90° or 270°. 190.5 1860.0 ANT MODE VOL Outer Knob PWR ADF BRG TUNE ADF - Standard direction finding mode.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CDF-552 Controls (Series III and FliteLine Interface continued…) CHELTON ADF Mode Selector Continued… BFO - (Beat Frequency Oscillator) ACT 1 190.5 Identical to ADF mode, but adds a 1,000-Hz tone to audio. L 15 Used only to identify interrupted-carrier signals (also known as cw). ADF BRG BFO MODE VOL Outer Knob TUNE PWR CHELTON ADF ACT 1 TST - Test Mode 1. Sends a park-at-90° command to external indicators. 190.5 2.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CDF-552 Controls (Series III and FliteLine Interface continued…) Volume Control CHELTON ADF ACT 1 VOLUME - (inner knob of MODE SELECTOR). Controls audio level of receiver. 190.5 1860.0 ANT ADF BRG MODE VOL Inner Knob TUNE PWR CHELTON Frequency Knobs ADF ACT 1 Large (right outer) knob tunes the receive frequency in hundreds of kHz from 100kHz through 2100kHz, skipping 1900kHz and 2000kHz. 190.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CDF-552 Controls (Series III and FliteLine Interface continued…) CHELTON ACT 1 When the large knob is rotated clockwise from 18 to the next detent, 2100 will appear in the display. Next, rotating the small knob one detent clockwise will cause 2182 to appear in the display. The small knob may then be used to tune from 2181 through 2183 about the maritime emergency frequency of 2182 kHz. ADF 2182.0 2100.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CDF-552 Controls (Series III and FliteLine Interface continued…) CHELTON ACT 1 FREQUENCY TRANSFER ADF The right inner knob also acts as a momentary pushbutton switch. Pressing and immediately releasing exchanges the active and standby frequencies when both are displayed. 1860 Pressing and holding for two seconds before releasing temporarily removes the standby frequency. This allows the active frequency to be changed.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CDF-552 Controls (Series III and FliteLine Interface continued…) ACT 1 190.5 1860.0 ANT ACT 1 ADF The top line of the display is always the active frequency, indicated by the letters ACT. The number 1 or 2 below the letters ACT indicate the ADF System Number when more than one system is installed. Data in the lower line of the display depends on position of FUNCTION SELECTOR.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CDF-552 Controls (Series III and FliteLine Interface – Failure Indication) Dashes indicate a flag condition. ACT 1 -- ANT ADF BRG NOTE: FAIL 1, FAIL 2 or FAIL 3, 4, 5, 6, Annunciation indicates a System fault; the system is not usable in these conditions. ACT 1 FAIL 1 ANT Page 42 Dec 2005 ADF BRG Publication No. 150-047012 Rev.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CDF-552 Controls (BCD Interface) CHELTON Mode Selector ADF ACT 1 ANT - Enables the ADF System and the non-directional sense antenna. The last frequencies displayed reappear on the display. Frequency tuning is enabled, but no direction-finding capability exists in this mode. External pointers park horizontally. Volume may be adjusted for comfortable reception. 190.5 1749.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CDF-552 Controls (BCD Interface continued…) CHELTON ADF ACT 1 TST - Test Mode 1. Outputs a Test or Self Test discrete Signal to the radio. Active and Standby tuning are both available in this mode. 190.5 Note 1: The function of the Test/Self Test signal varies with regard to the installed radio. Please refer to the operation manual specific to the radio. 1749.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE Operating the CDF-552 Series III and Fliteline Interface 1. Set the MODE SELECTOR to ANT. Note that the external ADF pointer moves to 90° and stops. 2. If frequencies displayed are not the ones desired, rotate the FREQUENCY KNOBS until the desired frequency is displayed on the bottom line of the display. 3. Press and release the FREQUENCY TRANSFER button. This exchanges the two displayed frequencies. The desired frequency is now active. 4.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CDF-552 Notes 1. The FREQUENCY SELECTOR knobs tune the radio receiver directly. The display actually shows the frequencies to which the receiver is tuned. In addition to rotation of the FREQUENCY SELECTOR KNOBS, the receiver may be tuned by an external ARINC 429 digital bus. 2. Display intensity and panel lighting are controlled by external dimmer controls. 3.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE ADF System Block Diagram (Typical) VCO ±14V 10.7MHz IF Antenna HSI RMI EFIS Etc.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE FliteLine Dual VHF COM and VHF NAV Control Display System General Description The Chelton CCN-955 Com/Nav Control Display Unit combines the capabilities of the CVC-152 and CVN-252 Control Displays. The CCN-955 splits the screen displaying the communication transceiver data on the upper half and the navigational data on the lower half. Despite combining the two radio functions all functionality remains operationally equivalent.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CCN-955 Control Display Unit Active COM Frequency "Acitve" COM Annunciator COM System Number COM Tuning Annunciator COM Transmit Annunciator "Acitve" NAV Annunciator NAV System Number CHELTON StandbyCOM Frequency COM/NAV COM Volume Annunciator C ACT 124.950 12 O TX 134.750 25k 8.33k TST M N ACT 108.15 12 A 110.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CCN-955 Controls Page 50 Dec 2005 C ACT 124.950 1 O 121.500 M 25k 8.33k TST N ACT 110.20 1 A 108.15 ON RAD BRG V COM Tuning C ACT 124.950 1 O 121.500 M 25k 8.33k TST N ACT 110.20 1 A 108.15 ON RAD BRG V NAV Tuning Indicates that the Communications transceiver is the selected radio system. The left inner knob acts as a momentary pushbutton that selects operation of the COM or NAV Functions.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE Operating the CCN-955 1. Operation of the CCN-955 is fundamentally the same as operating individual COM and NAV Units 2. The left inner knob acts as a momentary pushbutton that selects operation of the COM or NAV Functions. * this pushbutton is also the power (PWR) pushbutton Publication No. 150-047012 Rev.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CCN-955 Notes 1. Refer to the CVC-152 section for instructions on COM operation. 2. Refer to the CVN-252 section for instructions on NAV operation. 3. Pressing and holding the left pushbutton (PWR) for more than 1 second will trigger the system to shutdown. A warning screen will display a countdown. Releasing the PWR button before the count has expired will return the unit to the display screen active prior to initiating the shutdown.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE FliteLine ATC Transponder System (FliteXPDR) General Description CTR-352 The CTR-352 Control Display Unit provides a simultaneous control of up to two Mode A/C transponders. The CTR-352 Control display provides tuning of the ATC 4096 Code with a special VFR Quicktune feature to rapidly change the ATC code to 1200. The IDENT Annunciator (ID) appears in the display when the Transponder is replying to interrogation from the ATC ground station.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CTR-352 Control Display Unit CHELTON ATC ATC Label ATC Code ATC ATC System Number 1200 1 ATC Mode Annunciators IDENT Reply/Ident Lamp TST Mode Select (Outer Knob) Cursor Control (Inner Knob) Power On/OFF (pushbutton) MODE PWR SEL SBY ON ALT TUNE Code Upper Digits (Outer Knob) Transponder ID Select (Outer Knob) Code Lower Digits (Inner Knob) Transponder ID Select (Inner Knob) VFR Code 1200 Select (pushbutton) IDENT (pushbutton) Page 54 Dec 2005 Pu
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CTR-352 Controls (ARINC-410 Octal Interface) CHELTON Mode Selector ATC ON – Transponder ON ATC 1 The selected Transponder is ON (active), and reports the indicated code when interrogated (Mode A).
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CTR-352 Controls (ARINC-410 Octal Interface continued…) CHELTON ATC TST - Test Mode 1. Outputs a Test or Self Test discrete Signal to the radio. ATC 1200 1 TST SBY ON Note 1: The function of the Test/Self Test signal varies with regard to the installed radio. Please refer to the operation manual specific to the radio. Note 2: The code may be changed while in Test Mode. ALT TUNE MODE PWR SEL Outer Knob Note 3.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE ATC CODE CONTROL CHELTON If the Cursor is focused on the ATC Code field, changes of the right inner knob will change the two lower digits of the display. ATC Changes of the right outer knob will change the two upper digits of the display. ATC 1200 1 TST SBY ON Note: Clockwise rotation increases the number while counter-clockwise rotation will decrease the number.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CHELTON ATC TRANSPONDER SELECTION If the Cursor is focused on the Selected Transponder Id field, changes of the right inner or outer knob will change the displayed Selected Transponder Id. ATC 2 1200 Note: The Cursor will return to the ATC Code field after 5 seconds of inactivity on any other field.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CHELTON SPECIAL ATC CODES ATC 1200 – VFR Code for any altitude 7500 - Hijack Mode ATC 1 TST 7600 – Loss of Communications 7700 SBY ON MODE 7700 – Emergency (received by secondary surveillance radio sites at all times. ALT TUNE Note: 7500, 7600, and 7700 Codes are annunciated with a red background as they indicate a critical condition.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE Operating the CTR-352 ARINC-410 (Octal) Interface 1. Set the MODE SELECTOR to ON. 2. If the code displayed is not the one desired, rotate the CURSOR CONTROL until the ATC Code surrounds CURSOR BOX. Rotate the right inner knob to adjust the lower two digits from 00-77. Rotate the right outer knob to adjust the upper two digits from 00-77. 3. If the VFR code is desired press and hold the right pushbutton until “1200” is displayed. 4.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE CTR-352 Notes 1. When changing the ATC code, care should be made so as to avoid inadvertently selection of codes 7500, 7600, and 7700. For example, tuning upwards from 2700 to 7200 (rather than downward which would pass through the emergency frequencies) will help avoid triggering automated grounds stations. 2. Pressing and holding the left pushbutton (PWR) for more than 1 second will trigger the system to shutdown. A warning screen will display a countdown.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE ATC System Block Diagram (Typical) ANTENNA Pressure Encoding Altimeter ATC Transponder 1 CTR-352 ANTENNA ATC Transponder 2 Pressure Encoding Altimeter Page 62 Dec 2005 Publication No. 150-047012 Rev.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE FliteLogic EFIS Tuning Features General Description The CVC-152, CVN-252, and CCN-955 are designed to integrate with the Chelton FliteLogic Electronics Flight Instrument System (EFIS). The Control Displays receive COM and NAV tuning frequencies from the EFIS database to reduce pilot workload. Operating the Control Displays with EFIS 1. On the EFIS, display the information for the facility (see Waypoint Information (NavData), page 5-38 EFIS Manual). 2.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE Configuration Status Page (all units) The Configuration Status Page offers the pilot an efficient means to verify the installation options that affect the user operation of the Control Display. For additional information refer to the Installation Manual, FliteLine Control Displays, Part Number 150-047011.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE Options for Status Items on General Page: UNIT TYPE S GENERAL COM/NAV T UNIT TYPE NAV COM A NVG NO NAV VOLUME YES ADF T LIGHTING 5VAC Notes: U DME HOLD NO S INTERFACE SERIES III ARINC 410 FLITELINE NVG YES NO DME HOLD YES NO LIGHTING 5VDC 28VDC 5VAC VOLUME YES NO The DME HOLD field applies only to the CCN-955 and CVN-252. Options for Status Items on Interface Page: INTERFACE COM FREQ S INTERFACE Series III RANGE A (118.000-151.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE Limitations DME hold must be prominently displayed in the normal forward field of view of the flight crew any time DME HOLD is selected. Page 66 Dec 2005 Publication No. 150-047012 Rev.
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FLITELINE AVIONICS SYSTEM PILOT’S GUIDE This page intentionally left blank. Publication No. 150-047012 Rev.